View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 56710U 26145.39485903 +.00000000 +00000-0 +70129-4 0 00004
2 56710 87.9175 278.9873 0002066 88.4043 271.7327 13.20772463 07
| Epoch (UTC): | 25 May 2026 09:28:35 |
| Eccentricity: | 0.0002066 |
| inclination: | 87.9175° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9873° |
| argument of perigee: | 88.4043° |
| revolutions per day: | 13.20772463 |
| mean anomaly at epoch: | 271.7327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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